Turbocharger control

• US 4,177,006 A
• Filed: 09/29/1977
• Issued: 12/04/1979
• Est. Priority Date: 09/29/1977
• Status: Expired due to Term

• Current Assignee: The Garrett Corporation
• Original Assignee: The Garrett Corporation
• Inventors: Nancarrow, James H.
• Primary Examiner(s): Casaregola, Louis J.
• Application Number:
  US05/837,799
• Time in Patent Office: 796 Days
• Field of Search: 415/205, 415/151, 417/407, 60/605, 60/602
• US Class Current: 415/151
• CPC Class Codes: F02B 37/025 Multiple scrolls or multiple gas passages guiding the gas to the pump drive
• CPC Class Codes: F02B 37/22 by varying cross-section of exhaust passages or air passages , e.g. by throttling turbine inlets or outlets or by varying effective number of guide conduits F02B37/24 takes precedence
• CPC Class Codes: Y02T 10/12 Improving ICE efficiencies

Abstract

A variable flow geometry, meridionally divided turbine housing for use in an exhaust gas driven turbine of a turbocharger.

Claims

1. A turbocharger comprising a compressor;

and a fluid driven turbine drivingly coupled to said compressor, said turbine including a turbine housing having a fluid inlet portion and a generally scroll-shaped portion, a radially inwardly extending meridonal septum dividing said inlet and scroll-shaped portions into a pair of axially displaced primary fluid flow paths, wall means formed integrally with said turbine housing for closing a portion of the radially inner boundary of said primary paths and for defining a radially inwardly open secondary flow path in communication with said primary paths, and valve means disposed along the secondary flow path and controllably movable between a first position opening said secondary path to allow fluid flow through both said primary and secondary paths, and a second position substantially closing said secondary path to fluid flow.

2. A turbocharger as set forth in claim 1 wherein said wall means includes a radially inwardly extending meridional septum dividing said secondary flow path into a pair of substantially similar secondary flow passages.

3. A turbocharger as set forth in claim 1 wherein said scroll-shaped portion extends from said inlet portion with a continuously decreasing size, and said wall means closes the radially inner boundary of said primary flow paths over about 90°

generally at the upstream end of said scroll-shaped portion.

4. A turbocharger as set forth in claim 1 wherein said primary flow paths are substantially identical.

5. A turbocharger as set forth in claim 2 wherein said valve means includes means disposed along each of said secondary passages for uniform and simultaneous movement between said first and second positions.

6. A turbocharger as set forth in claim 5 wherein said valve means is disposed generally at the upstream ends of said secondary passages.

7. A turbocharger as set forth in claim 1 wherein said valve means comprises a sleeve mounted on said turbine housing along said secondary path and having flow openings to permit fluid flow through said sleeve and secondary path, and a valve insert movably carried within said sleeve for selectively controlling fluid flow through the flow openings in said sleeve.

8. A turbocharger as set forth in claim 2 wherein said valve means comprises a sleeve mounted on said turbine housing along said secondary passages and having flow openings disposed in each of said passages to permit fluid flow through said sleeve and said secondary passages, and a valve insert movably carried within said sleeve for selectively controlling fluid flow through the flow openings.

9. A turbocharger as set forth in claim 2 wherein said valve means includes means for controllably opening and limiting one of said secondary passages to fluid flow in one of said primary paths, and for controllably opening and limiting the other of said secondary passages to fluid flow in the other of said primary paths.

10. A turbocharger as set forth in claim 2 wherein said valve means includes means disposed in both of said secondary passages for controllably and together opening and limiting said secondary passages to fluid flow.

11. A turbocharger as set forth in claim 1 including actuator means for controllably adjusting the position of said valve means.

12. A turbocharger as set forth in claim 2 wherein said valve means comprises a sleeve mounted on said turbine housing generally at the upstream ends of said secondary passages and having flow openings to permit fluid flow through said sleeve and said secondary passages, and a valve insert having a generally semicircular cross section movably received within said sleeve for selectively controlling fluid flow through the flow openings, said insert including means for maintaining separate the flow through said secondary passages.

13. A turbocharger comprising a compressor;

and a fluid driven turbine drivingly coupled to said compressor, said turbine including a turbine housing having a fluid inlet portion and a generally scroll-shaped portion, a radially inwardly extending meridional septum dividing said inlet and scroll-shaped portions into a pair of axially displaced primary fluid flow paths, wall means formed integrally with said turbine housing for closing a portion of the radially inner boundary of said primary paths and having means extending radially inwardly therefrom for defining a pair of radially inwardly open secondary flow passages open to respective ones of said primary paths, and valve means disposed along the secondary flow passages and controllably movable between a first position opening said secondary passages to their respective primary paths to allow fluid flow both through said primary paths and secondary passages, and a second position substantially closing said secondary passages to fluid flow.

14. A turbocharger as set forth in claim 13 wherein said wall means closes a portion of the radially inner boundary of said primary paths generally at the upstream end of said scroll-shaped portion.

15. A turbocharger as set forth in claim 13 wherein said valve means comprises a sleeve mounted on said turbine housing along said secondary passages and having flow openings disposed in each of said passages to permit fluid flow through said sleeve and said secondary passages, and a valve insert movably carried within said sleeve for selectively controlling fluid flow through the flow openings.

16. A turbocharger as set forth in claim 13 wherein said valve means includes means disposed in both of said secondary passages for controllably and together opening and limiting said secondary passages to fluid flow.

17. A turbocharger comprising a compressor;

and a fluid driven turbine drivingly coupled to said compressor, said turbine including a turbine housing having a fluid inlet portion and a generally scroll-shaped portion, a radially inwardly extending meridional septum dividing said inlet and scroll-shaped portions into a pair of axially displaced primary fluid flow paths, wall means formed integrally with said turbine housing for closing a portion of the radially inner boundary of said primary paths and having means extending radially inwardly therefrom for defining a pair of radially inwardly open secondary flow passages in communication with the primary paths, and valve means disposed along each of said secondary passages and controllably movable between a first position opening said secondary passages to fluid flow in respective ones of said primary paths to allow fluid flow both through said primary paths and secondary passages, and a second position uniformly and substantially closing said secondary passages to fluid flow.

18. A turbine housing for a turbomachine comprising a fluid inlet portion;

a generally scroll-shaped portion joined to said inlet portion;

a radially inwardly directed meridional septum extending along said inlet and scroll portions to define a pair of axially displaced primary fluid flow paths;

wall means formed integrally with the housing for closing a portion of the radially inner boundary of said primary paths and for defining a radially inwardly open secondary flow path in communication with the primary paths; and

valve means disposed along the secondary flow path and controllably movable between a first position opening said secondary path to said primary paths to allow fluid flow both through said primary and secondary paths, and a second position substantially closing said secondary path to fluid flow.

19. A turbine housing as set forth in claim 18 wherein said wall means includes a radially inwardly extending meridional septum dividing said secondary flow path into a pair of substantially similar secondary flow passages, said secondary flow passages being for communicating with respective ones of said primary paths.

20. A turbine housing as set forth in claim 19 wherein said valve means comprises a sleeve mounted on said turbine housing along said secondary passages and having flow openings disposed in each of said passages to permit fluid flow through said sleeve and said secondary passages, and a valve insert movably carried within said sleeve for selectively controlling fluid flow through the flow openings.

21. A turbine housing as set forth in claim 19 wherein said valve means includes means disposed in both of said secondary passages for controllably and together opening and limiting said secondary passages to fluid flow.

22. In a meridionally divided turbine housing having a pair of axially displaced primary flow paths formed along a fluid inlet portion and a generally scroll-shaped portion, apparatus for varying the housing fluid flow geometry comprising wall means fixed with respect to the turbine housing and forming a relatively short, radially inwardly open secondary fluid flow path open to said primary paths;

and valve means disposed along said secondary path and controllably movable between a first position opening said secondary path to allow fluid flow both through said primary and secondary paths, and a second position substantially closing said secondary path to fluid flow.

23. Apparatus as set forth in claim 22 wherein said means forming said secondary path comprises wall means for closing a portion of the radially inner boundary of said primary paths and including a radially inwardly extending septum defining a path of radially inwardly open secondary flow passages open to respective ones of said primary paths.

24. Apparatus as set forth in claim 23 wherein said valve means includes means disposed in both of said secondary passages for controllably and together opening and limiting said secondary passages to fluid flow.

25. A method of controlling fluid flow through a turbine housing having a fluid inlet portion and a generally scroll-shaped portion, comprising the steps of dividing said inlet and scroll portions with a radially inwardly extending meridional septum to form a pair of axially displaced primary flow paths;

closing the radially inner boundary of a portion of said primary paths with wall means fixed with respect to the turbine housing to form a radially inwardly open secondary flow path in communication with said primary paths; and

controllably adjusting the valve means disposed along said secondary path between a first position opening said secondary path to allow fluid flow both through said primary and secondary paths, and a second position substantially closing said secondary path to fluid flow to allow unrestricted fluid flow through said primary paths.

26. The method of claim 25 including the step of meridionally dividing said secondary path into a pair of substantially similar secondary passages in communication with respective ones of said primary paths.

27. The method of claim 26 wherein said step of controllably adjusting said valve means comprises adjusting said valve means to controllably open and limit said secondary passages together.

28. The method of claim 25 wherein said closing step comprises closing a portion of the radially inner boundary of said primary paths generally at the upstream end of said scroll portion.

29. A method of controlling fluid flow through a turbine housing having a fluid inlet portion and a generally scroll-shaped portion, comprising the steps of dividing said inlet and scroll portions with a radially inwardly extending meridional septum to form a pair of axially displaced primary flow paths;

closing the radially inner boundary of a portion of said primary paths with wall means formed integrally with the turbine housing to form a pair of radially inwardly open secondary flow passages in communication with respective ones of said primary paths; and

controllably adjusting valve means disposed along said secondary passages between a first position opening said secondary passages to fluid flow to allow fluid flow both through said primary paths and secondary passages, and a second position substantially closing said secondary passages to fluid flow to allow unrestricted fluid flow only through said primary paths.

30. In a meridionally divided turbine housing having a pair of axially displaced primary fluid flow paths formed along a fluid inlet portion and a generally scroll-shaped portion, a method of varying the housing fluid flow geometry comprising the steps of closing the radially inner boundary of a portion of the primary paths with wall means formed integrally with the turbine housing to form a relatively short, radially inwardly open secondary fluid flow path communicating with said primary paths;

and controllably adjusting valve means disposed along said secondary path between a first position opening said secondary path to allow fluid flow both through said primary and secondary paths, and a second position substantially closing said secondary path to fluid flow to allow unrestricted fluid flow only through the primary paths.

31. The method of claim 30 wherein said forming step comprises forming a pair of radially inwardly open secondary flow passages along said secondary path, said secondary passages being in communication with respective ones of said primary paths.

32. The method of claim 31 wherein said step of controllably adjusting said valve means comprises adjusting said valve means to controllably open and limit said secondary passages together.

33. A turbocharger comprising a compressor;

and a fluid driven turbine drivingly coupled to said compressor, said turbine including a turbine housing having a fluid inlet portion and a generally scroll-shaped portion, a radially inwardly extending meridional septum dividing said inlet and scroll-shaped portions into a pair of axially displaced primary fluid flow paths, wall means for closing a portion of the radially inner boundary of said primary paths and defining a radially inwardly open secondary flow path in communication with said primary paths, and valve means including a sleeve mounted on the turbine housing along said secondary path and having flow openings to permit fluid flow through said sleeve and secondary path, and a valve insert movably carried within said sleeve and controllably movable between a first position opening said sleeve and secondary path to allow fluid flow through said primary and secondary paths, and a second position limiting fluid flow through said sleeve and secondary path.

34. A turbocharger comprising a compressor;

and a fluid driven turbine drivingly coupled to said compressor, said turbine including a turbine housing having a fluid inlet portion and a generally scroll-shaped portion, a radially inwardly extending meridional septum dividing said inlet and scroll-shaped portions into a pair of axially displaced primary fluid flow paths, wall means for closing a portion of the radially inner boundary of said primary paths and having means extending radially inwardly therefrom defining a pair of radially inwardly open secondary flow passages open to respective ones of said primary paths, and valve means including a sleeve mounted on the turbine housing along said secondary passages and having flow openings disposed in each of said passages to permit fluid flow through said sleeve and said secondary passages, and a valve insert movably carried within said sleeve and controllably movable between a first position opening said sleeve flow openings and secondary passages to their respective primary paths to allow fluid flow through said primary paths and secondary passages, and a second position limiting fluid flow through said sleeve flow openings and secondary passages.

35. A turbocharger as set forth in claim 34 wherein said valve insert includes means for maintaining separate the flow through said secondary passages.

36. A turbocharger comprising a compressor;

and a fluid driven turbine drivingly coupled to said compressor, said turbine including a turbine housing having a fluid inlet portion and a generally scroll-shaped portion, a radially inwardly extending meridional septum dividing said inlet and scroll-shaped portions into a pair of axially displaced primary fluid flow paths, wall means for closing a portion of the radially inner boundary of said primary paths and having means extending radially inwardly therefrom defining a pair of radially inwardly open secondary flow passages, and valve means including a sleeve mounted on the housing along each of said secondary passages and having flow openings disposed in each of said passages to permit fluid flow through said sleeve and said passages, and a valve insert movably carried within said sleeve and controllably movable between a first position opening said sleeve flow openings and secondary passages to fluid flow in respective ones of said primary paths to allow fluid flow through said primary paths and secondary passages, and a second position uniformly limiting fluid flow through said sleeve flow openings and secondary passages.